View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20804U 90083A 23082.90664921 .00000091 00000-0 80717-4 0 9993
2 20804 82.9404 322.5315 0036314 332.4973 37.8077 13.74393460630968
Epoch (UTC): | 23 March 2023 21:45:34 |
Eccentricity: | 0.0036314 |
inclination: | 82.9404° |
perigee height: | 957 km |
apogee height: | 1010 km |
right ascension of ascending node: | 322.5315° |
argument of perigee: | 332.4973° |
revolutions per day: | 13.74393460 |
mean anomaly at epoch: | 37.8077° |
orbit number at epoch: | 63096 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|